Embodiments of the invention relate to tilting pad bearing assemblies and apparatuses. The disclosed tilting pad bearing assemblies and apparatuses may be employed in downhole motors of a subterranean drilling system or other mechanical systems. In an embodiment, a bearing assembly or apparatus includes a support ring and a plurality of tilting pads. Each tilting pad is tilted and/or tiltably secured relative to the support ring. In some embodiments, one or more of the tilting pads include a plurality of superhard bearing segments assembled to form a superhard bearing surface. One or more seams may be positioned between adjacent superhard bearing segments of the superhard bearing segments. In other embodiments, one or more of the tilting pads may include at least one or only one superhard bearing segment, such as a polycrystalline diamond bearing segment.
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1. A bearing apparatus, comprising:
a first bearing assembly including one or more first superhard bearing segments having one or more first superhard bearing surfaces; and
a second bearing assembly including:
a support ring; and
a plurality of tilting pads each of which is tilted and/or tiltably secured relative to the support ring, each of the plurality of tilting pads including:
a plurality of second superhard bearing segments assembled to form a substantially continuous second superhard bearing surface generally opposing the one or more first superhard bearing surfaces of the first bearing assembly, one or more seams positioned between adjacent second superhard bearing segments of the plurality of second superhard bearing segments.
19. A bearing apparatus, comprising:
a stator including one or more first polycrystalline diamond bearing segments having one or more first superhard bearing surfaces; and
a rotor including:
a support ring; and
a plurality of tilting pads each of which is tilted and/or tiltably secured relative to the support ring, each of the plurality of tilting pads including:
a plurality of second polycrystalline diamond bearing segments that collectively define a substantially continuous second superhard bearing surface generally opposing the one or more first superhard bearing surfaces of the stator, one or more seams positioned between adjacent second polycrystalline diamond bearing segments of the plurality of second polycrystalline diamond bearing segments.
21. A rotating machine, comprising:
a motor operable to apply torque to a rotary drill bit, the motor operably coupled to a thrust-bearing apparatus, the thrust-bearing apparatus including:
a stator including one or more first polycrystalline diamond bearing segments having one or more first superhard bearing surfaces; and
a rotor including:
a support ring; and
a plurality of tilting pads each of which is tilted and/or tiltably secured relative to the support ring, each of the plurality of tilting pads including:
a plurality of second polycrystalline diamond bearing segments assembled to form a substantially continuous second superhard bearing surface generally opposing the one or more first superhard bearing surfaces of the stator, one or more seams positioned between adjacent second polycrystalline diamond bearing segments of the plurality of second polycrystalline diamond bearing segments.
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22. The rotating machine of
23. The rotating machine of
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This application is a continuation of U.S. application Ser. No. 13/089,725 filed on 19 Apr. 2011, the disclosure of which is incorporated herein, in its entirety, by this reference.
Wear-resistant, superhard compacts are utilized in a variety of mechanical applications. For example, polycrystalline diamond compacts (“PDCs”) are used in drilling tools (e.g., cutting elements, gage trimmers, etc.), machining equipment, bearing apparatuses, wire-drawing machinery, and in other mechanical apparatuses.
PDCs have found particular utility as superhard bearing elements in fixed-position thrust bearings within subterranean drilling systems. A PDC bearing element typically includes a superhard diamond layer commonly referred to as a diamond table. The diamond table is formed and bonded to a substrate using a high-pressure/high-temperature (“HPHT”) process.
A fixed-position thrust-bearing apparatus includes a number of PDC bearing elements affixed to a support ring. The PDC bearing elements bear against PDC bearing elements of an adjacent bearing assembly during use. PDC bearing elements are typically brazed directly into a preformed recess formed in a support ring of a fixed-position thrust bearing.
Embodiments of the invention relate to bearing assemblies and apparatuses, which may be operated hydrodynamically. The disclosed bearing assemblies and apparatuses may be employed in bearing apparatuses for use in downhole motors of a subterranean drilling system or other mechanical systems.
In one or more embodiments, a bearing assembly includes a support ring and a plurality of tilting pads. Each tilting pad is tilted and/or tiltably secured relative to the support ring. In some embodiments, one or more of the tilting pads include a plurality of superhard bearing segments assembled to form a superhard bearing surface. One or more seams may be formed and positioned between adjacent superhard bearing segments of the superhard bearing segments. In other embodiments, one or more of the tilting pads may include at least one or only one superhard bearing segment, such as a polycrystalline diamond (“PCD”) bearing segment.
In an embodiment, a bearing apparatus includes a rotor and a stator. The rotor or stator may include any of the bearing assembly embodiments disclosed herein.
Other embodiments are directed to motor assemblies including any of the bearing assembly and apparatus embodiments disclosed herein.
Features from any of the disclosed embodiments may be used in combination with one another, without limitation. In addition, other features and advantages of the present disclosure will become apparent to those of ordinary skill in the art through consideration of the following detailed description and the accompanying drawings.
The drawings illustrate several embodiments of the present disclosure, wherein identical reference numerals refer to identical or similar elements or features in different views or embodiments shown in the drawings.
Embodiments of the invention relate to tilting pad bearing assemblies and apparatuses, which may be operated hydrodynamically. The disclosed tilting pad bearing assemblies and apparatuses may be employed in downhole motors of a subterranean drilling system or other mechanical systems. Motor assemblies including at least one of such bearing assemblies or apparatus are also disclosed, as well as methods of fabricating such bearing assemblies and apparatuses utilizing superhard compacts.
While the description herein provides examples relative to a subterranean drilling and motor assembly, the tilting pad bearing assembly and apparatus embodiments disclosed herein may be used in any number of applications. For instance, tilting pad bearing assemblies and apparatuses may be used in pumps, motors, compressors, turbines, generators, gearboxes, and other systems and apparatuses, or in any combination of the foregoing. Furthermore, while the embodiments disclosed herein are described as being operated hydrodynamically, the tilting pad bearing assemblies and apparatuses may also be operated partially hydrodynamically or not hydrodynamically, if desired or needed.
The tilting pads 104 of the illustrated embodiment generally have a truncated pie-shaped geometry or a generally trapezoidal geometry, and may be distributed about a thrust axis 106, along which a thrust force may be generally directed during use. Each tilting pad 104 may be located circumferentially adjacent to another tilting pad 104, with a gap 108 or other offset therebetween. For instance, the gap 108 may separate adjacent tilting pads 104 by a distance of about 2.0 mm to about 20.0 mm, or more particularly a distance of about 3.5 mm to about 15 mm, although the separation distance may be greater or smaller. For instance, as the size of the hydrodynamic tilting pad bearing assembly 100 increases, the size of the tilting pads 104 and/or the size of the gaps 108 may also increase. Each tilting pad 104 includes a discrete superhard bearing surface 116, such that the tilting pads 104 collectively provide a non-continuous superhard bearing surface. The term “superhard,” as used herein, means a material having a hardness at least equal to a hardness of tungsten carbide.
To support the tilting pads 104 of the bearing assembly 100, the support ring 102 may define a channel 110 and the tilting pads 104 may be placed within the channel 110. In other embodiments, the support ring 102 may define multiple pockets or otherwise define locations for the tilting pads 104. The tilting pads 104 may then be supported or secured within the support ring 102 in any suitable manner. For instance, as discussed hereafter, a pivotal connection may be used to secure the tilting pads 104 within the support ring 102, although any other suitable securement or attachment mechanism may also be utilized. The support ring 102 may also include an inner, peripheral surface defining an aperture 114. The aperture 114 may be generally centered about the thrust axis 106, and may be adapted to receive a shaft (e.g., a downhole drilling motor shaft).
As best shown in
Each tilting pad 104 optionally includes multiple layers or other components. For instance, each segment of the tilting pad 104 may be a superhard compact that includes a superhard table 118 bonded to a substrate 120. The superhard table 118 may be at least partially made from a number of different superhard materials. Suitable materials for use in the superhard table 118 include natural diamond, sintered PCD, polycrystalline cubic boron nitride, diamond grains bonded together with silicon carbide, or combinations of the foregoing. In an embodiment, the superhard table 118 is a PCD table that includes a plurality of directly bonded-together diamond grains exhibiting diamond-to-diamond bonding therebetween (e.g., sp3 bonding), which define a plurality of interstitial regions. A portion of, or substantially all of, the interstitial regions of such a superhard table 118 may include a metal-solvent catalyst or a metallic infiltrant disposed therein that is infiltrated from the substrate 120 or from another source. For example, the metal-solvent catalyst or metallic infiltrant may be selected from iron, nickel, cobalt, and alloys of the foregoing. The superhard table 118 may further include thermally-stable diamond in which the metal-solvent catalyst or metallic infiltrant has been partially or substantially completely depleted from a selected surface or volume of the superhard table 118 using, for example, an acid leaching process.
For example, appropriately configured PDCs may be used as the tilting pads 104, which may be formed in an HPHT processes. For example, diamond particles may be disposed adjacent to the substrate 120, and subjected to an HPHT process to sinter the diamond particles to form a PCD table that bonds to the substrate thereby forming the PDC. The temperature of the HPHT process may be at least about 1000° C. (e.g., about 1200° C. to about 1600° C.) and the cell pressure of the HPHT process may be at least 4.0 GPa (e.g., about 5.0 GPa to about 12 GPa or about 7.5 GPa to about 11 GPa) for a time sufficient to sinter the diamond particles.
The diamond particles may exhibit an average particle size of about 50 μm or less, such as about 30 μm or less, about 20 μm or less, about 10 μm to about 18 μm, or about 15 μm to about 18 μm. In some embodiments, the average particle size of the diamond particles may be about 10 μm or less, such as about 2 μm to about 5 μm or submicron. In some embodiments, the diamond particles may comprise a relatively larger size and at least one relatively smaller size. As used herein, the phrases “relatively larger” and “relatively smaller” refer to particle sizes (by any suitable method) that differ by at least a factor of two (e.g., 30 μm and 15 μm). According to various embodiments, the mass of diamond particles may include a portion exhibiting a relatively larger size (e.g., 30 μm, 20 μm, 15 μm, 12 μm, 10 μm, 8 μm) and another portion exhibiting at least one relatively smaller size (e.g., 6 μm, 5 μm, 4 μm, 3 μm, 2 μm, 1 μm, 0.5 μm, less than 0.5 μm, 0.1 μm, less than 0.1 μm). In one embodiment, the diamond particles may include a portion exhibiting a relatively larger size between about 10 μm and about 40 μm and another portion exhibiting a relatively smaller size between about 1 μm and 4 μm. In some embodiments, the diamond particles may comprise three or more different sizes (e.g., one relatively larger size and two or more relatively smaller sizes), without limitation. The PCD table so-formed after sintering may exhibit an average diamond grain size that is the same or similar to any of the foregoing diamond particle sizes and distributions.
In some embodiments, one or more sp2-carbon-containing additives may be mixed with the diamond particles. For example, the one or more sp2-carbon-containing additives may be present in a mixture with the diamond particles in an amount of about 1 weight percent (“wt %”) to about 15 wt %, such as 3 wt % to about 12 wt %, about 4.5 wt % to about 6.5 wt %, about 4.5 wt % to about 5.5 wt, or about 5 wt % of the mixture. The one or more sp2-carbon-containing additives may be chosen from graphite, graphene, fullerenes, ultra-dispersed diamond particles, or combinations of the foregoing.
In an embodiment, the superhard table 118 may be integrally formed with the substrate 120. For example, the superhard table 118 may be a sintered PCD table that is integrally formed with the substrate 120. In such an embodiment, the infiltrated metal-solvent catalyst may be used to catalyze formation of diamond-to-diamond bonding between diamond grains of the superhard table 118 from diamond powder during HPHT processing. In another embodiment, the superhard table 118 may be a pre-sintered superhard table that has been HPHT bonded to the substrate 120 in a second HPHT process after being initially formed in a first HPHT process. For example, the superhard table 118 may be a pre-sintered PCD table that has been leached to substantially completely remove metal-solvent catalyst used in the manufacture thereof and subsequently HPHT bonded or brazed to the substrate 120 in a separate process.
In some embodiments, the superhard table 118 may be leached to deplete a metal-solvent catalyst or a metallic infiltrant therefrom in order to enhance the thermal stability of the superhard table 118. For example, where the superhard table 118 is a PCD table, the superhard table 118 may be leached to remove at least a portion of the metal-solvent catalyst from a working region thereof to a selected depth that was used to initially sinter the diamond grains to form a leached thermally-stable region. The leached thermally-stable region may extend inwardly from the superhard bearing surface 116 to a selected depth. In one example, the depth of the thermally-stable region may be about 10 μm to about 500 μm. More specifically, in some embodiments, the selected depth is about 50 μm to about 100 μm or about 200 μm to about 350 μm. The leaching may be performed in a suitable acid, such as aqua regia, nitric acid, hydrofluoric acid, or mixtures of the foregoing.
The substrate 120 may similarly be formed from any number of different materials, and may be integrally formed with, or otherwise bonded or connected to, the superhard table 118. Materials suitable for the substrate 120 may include, without limitation, cemented carbides, such as tungsten carbide, titanium carbide, chromium carbide, niobium carbide, tantalum carbide, vanadium carbide, or combinations thereof cemented with iron, nickel, cobalt, or alloys thereof. For example, in an embodiment, the substrate 120 comprises cobalt-cemented tungsten carbide. However, in certain embodiments, the superhard tables 118 may be omitted, and each superhard bearing segment may be made from a superhard material, such as cemented tungsten carbide. In other embodiments, the substrate 120 may be omitted and the superhard bearing segment may be a superhard material, such as a polycrystalline diamond body that has been leached to deplete metal-solvent catalyst therefrom or may be an un-leached PCD body.
In the embodiment illustrated in
In the illustrated embodiment, the set of superhard bearing segments collectively defining at least a portion of the tilting pad 104 are secured to a support plate 122. The support plate 122 may, for instance, be formed of a metal, an alloy, a cemented carbide material, other material, or any combination thereof. The substrate 120 of the superhard bearing segments may be secured to the support plate 122 by brazing, welding, or other method. In some embodiments, the support plate 122 may define a pocket into which the superhard bearing segments may be assembled and/or positioned. In at least one embodiment, the support plate 122 has an integral construction such that a single segment may form substantially the full support plate 122, while multiple superhard bearing segments may be used to form the superhard bearing surface 116. In other embodiments, multiple segments of one or more materials may be used to form or define the support plate 122.
The degree to which the tilting pads 104 rotate or tilt may be varied in any suitable manner. For instance, in an embodiment, the tilting pads 104 may be tilted about respective radial axes that extend radially from the thrust axis 106 and through each respective tilting pad 104. In
The pin 124 may be used to allow the tilting pads 104 to selectively rotate. For instance, the tilting pads 104 may be self-establishing such that based on the lubricant used, the axial forces applied along the thrust axis, the rotational speed of the runner or hydrodynamic tilting pad bearing assembly 100, other factors, or combinations of the foregoing, the tilting pads 104 may automatically or otherwise adjust to a desired tilt or other orientation. In still other embodiments, the tilting pads 104 may be fixed at a particular tilt, or may be manually set to a particular tilt with or without being self-establishing.
Further, the pin 124 represents a single mechanism for facilitating rotation, translation, or other positioning of the tilting pads 104 so as to provide tilting pad superhard bearing surfaces 116. In other embodiments, other mechanisms may be used. By way of illustration, leveling links, pivotal rockers, spherical pivots, other elements, or any combination of the foregoing may also be used to facilitate positioning of the tilting pads 104 in a tilted configuration. In an embodiment, the support plate 122 may be used to facilitate rotation of a respective tilting pad 104. The support plate 122 may, for instance, be machined or otherwise formed to include a receptacle, an opening, or other structure into which the pin 124 may be at least partially received or secured. In embodiments in which the pin 124 is excluded, the support plate 122 may be machined or otherwise formed to include other components, such as spherical pivot, pivotal rocker, or leveling link interface. The support plate 122 may be formed of any suitable material, such as steel or other alloy; however, in some embodiments the support plate 122 is formed of a material that is relatively softer than the substrate 120, such that the support plate 122 may be relatively easily machined or formed into a desired shape or form. In other embodiments, the support plate 122 can be eliminated and the substrate 120 may be directly machined or formed to facilitate tilting of the tilting pad 104.
In some embodiments, the tilt axis of the tilting pads 104 is centered relative to the tilting pads 104. For instance, where the support ring 102 may be configured for bi-directional rotation, the tilt axis of the tilting pads 104 may be centered due to either of opposing edges of the tilting pads 104 being the leading or trailing edge, based on a particular direction of rotation. In other embodiments, the tilt axis of a tilting pad 104 may be offset relative to a center of the tilting pads 104. For instance, where the support ring 102 is part of a rotor configured for only unidirectional rotation, the axis of rotation of the tilting pad 104 may be offset such that the axis of rotation is closer to one of the leading edge or the trailing edge of the tilting pad 104. In other embodiments, a tilt axis may be offset from center despite a rotor being configured for bidirectional rotation, or a tilt axis may be centered despite a rotor being configured for unidirectional rotation.
The use of superhard materials such as those contemplated in the present disclosure may provide wear resistance, frictional, or other properties that extend the useful life and/or utility of the corresponding bearing, motor, or other assemblies described herein. For instance, in some applications, hardened steel bearing tilting pads may wear at a rate that is between five and twenty times greater than bearing pads made of superhard materials. Thus, in at least some applications, use of superhard materials in a tilting pad bearing assembly may significantly increase the potential useful life of a bearing assembly.
While superhard materials may thus provide desirable wear characteristics, use of some superhard materials may be limited in various regards. For instance, certain types of superhard materials may be manufacturable in limited quantities, or may be available with certain size restrictions. Such limitations may be the result of technological, quality, or economic constraints. For instance, in some cases, the technology to produce large pieces of a superhard material may not exist, or developing machinery that may produce large pieces may be cost prohibitive, or result in low quality components. PDCs are a superhard article including at least one such material that is considered to have production size constraints. For instance, as described herein, PDCs may be produced using an HPHT sintering and/or bonding process. To maintain the temperature and pressure requirements over a large surface area, and thereby produce large segments of PDCs, can consume large amounts of power and require large, powerful, and sophisticated machinery. If such pressure and temperature tolerances are not maintained, the PDCs may include defects that reduce desirable wear resistance and/or frictional characteristics of the PDCs. Moreover, the temperature and/or pressure requirements for production of a high quality and large PDC may exceed the capabilities of currently available HPHT presses. Consequently, PDCs are currently produced under size restrictions. For example, PDCs are available in limited sizes that typically range up to about 25 mm to about 75 mm (e.g., about 25 mm to about 30 mm) in diameter for cylindrical PDCs and up to about 3.0 mm in diamond table thickness.
Where the hydrodynamic tilting pad bearing assembly of
According to some embodiments, superhard materials such as polycrystalline diamond or PDCs including polycrystalline diamond may be formed as multiple independent superhard bearing segments that may be joined and/or assembled together to collectively define a superhard bearing element and/or superhard bearing surface.
In particular,
The illustrated embodiment shows an example structure of the superhard bearing segments 126a-f, and an example of how the superhard bearing segments 126a-f may be assembled together. In this embodiment, six superhard bearing segments 126a-f collectively define a pie-shaped bearing pad 126 and a substantially continuous superhard bearing surface 116, although more or fewer than six segments may be provided. Generally, more than one bearing segment may be provided to collectively form a tilting pad. Each superhard bearing segment 126a-f may include at least one outer edge region 132 and at least one interior edge region 134. In the illustrated embodiment, each outer edge region 132 defines a portion of a periphery of the superhard bearing surface 116. Each interior edge region 134 may be configured to correspond with, and in some embodiments may mesh with, corresponding interior edge regions of one or more of other of the superhard bearing segments 126a-f. In
In the illustrated embodiment, the superhard bearing surface 116 is substantially planar, although such embodiment is merely illustrative. In other embodiments, the superhard bearing surface 116 may be curved, or have another contour or topography. Moreover, the outer edges of the superhard bearing surface 116 optionally include a chamfer 140. The chamfer 140 may be formed by placing a chamfer on the individual outer edge regions 132 of each of the superhard bearing segments 126a-f. The superhard bearing surface 116 may also take a number of other forms. For instance, in
The superhard bearing segments 126a-f may also be arranged to each have any desired individual shape. By way of illustration, a set of seams 136 may be at least partially formed between separate superhard bearing segments 126a-f and each superhard bearing segment 126a-f may have a different size and/or shape. The superhard bearing segments 126a-f and/or seams 136 may be non-symmetrical. In other embodiments, however, the seams 136 and/or the superhard bearing segments 126a-f may define the superhard bearing surface 116 in a substantially symmetrical fashion.
Any number of superhard bearing segments may be used to form a superhard bearing surface 116. For instance, as noted above, a bearing tilting pad may be sized many times larger than a largest available size of a PDC or other material used to form a portion of the bearing tilting pad, or may be small enough to be formed of a single PDC. In
The interior edge regions 134 of the superhard bearing segments 126a-f may be configured to limit fluid from being able to leak through the seams 136 formed between adjacent superhard bearing segments 126a-f. By way of illustration, the seams 136 may be interconnected and defined by interfaces between the interior edge regions 134. Depending upon the tolerances of the superhard bearing segments 126a-f, all or a portion of the seams 136 may comprise a relatively small gap 138. For example, the gap 138 may have a width of about 0.001 mm to about 3.5 mm, more particularly a width of about 0.0025 mm to about 2.5 mm, and more particularly a width of about 0.125 mm to about 1.25 mm. More particularly still, the gap 138 may have a width from about 0.025 mm up to about 1.0 mm. In another embodiment, the gap 138 may have a width from about 0.005 mm up to about 0.50 mm. As the gaps 138 decrease in size, it may become more difficult for fluid to flow radially between the gaps 138 and leak from the superhard bearing surface 116 of the superhard bearing element 104. However, it should be noted that in at least some operational conditions, entrained fluid in the gaps 138 may assist with formation of a hydrodynamic film on the superhard bearing surface 116.
The interior edge regions 134 of the superhard bearing segments 126a-f in
The superhard bearing segments 226a-f of the illustrated embodiment each include interior edge regions 234 configured to correspond to and/or mate with interior edge regions 234 of two or three adjacent superhard bearing segments 226a-f. Each of the superhard bearing segments 226a-f may further include an outer edge region 232 defining at least a portion of the periphery of the superhard bearing surface 216. As discussed herein, the foregoing is merely an example. In other embodiments, there may be one or more superhard bearing segments that do not include an outer edge region, include an interior edge region corresponding to, or mating with, only one or more than three adjacent superhard bearing segments, or superhard bearing segments may have still other configurations.
In the illustrated embodiment, the superhard bearing segments 226a-f may include, at their respective interior edge regions 234, generally rectangular-shaped slots 250 and rectangular-shaped ridges 252. The slots 250 and ridges 252 may be configured to correspond to and potentially mesh with corresponding ridges 252 and slots 250 of adjoining segments 226a-f. Consequently, the superhard bearing segments 226a-f may at least partially interlock along respective interior edge regions 234.
Each superhard bearing segment 226a-f may thus be positioned radially, circumferentially, or otherwise adjacent to another of the superhard bearing segments 226a-f, with one of the seams 236 formed therebetween. In some embodiments, interlocked superhard bearing segments 226a-f may act to limit fluid leakage at the superhard bearing surface 216. For instance, the seams 236 may define a tortuous path to limit fluid leakage through the seams 236. If present, gaps located between adjacent superhard bearing segments 226a-f may further be filled with a sealant material to help limit leakage of fluid through the seams 236. For example, gaps between interior edge regions 234 may be substantially filled with a sealant material. Examples of sealant materials may include a ceramic material, metallic material, polymeric material, or another suitable material, or any combination of the foregoing. In an embodiment, the sealant material may exhibit abrasion and/or erosion resistance to commonly used drilling fluids (also known as drilling mud). For example, a sealant material may comprise chemically-vapor-deposited (“CVD”) diamond or a CVD-deposited carbide material (e.g., binderless tungsten carbide). Specifically, one example of a commercially available CVD binderless tungsten carbide material (currently marketed under the trademark HARDIDE®) is currently available from Hardide Layers Inc. of Houston, Tex.
In other embodiments, a binderless tungsten carbide material may be formed by physical vapor deposition (“PVD”), variants of PVD, high-velocity oxygen fuel (“HVOF”) thermal spray processes, supersonic transfer (“SST”), or any other suitable process, without limitation. In still other embodiments, the braze alloy used to braze the superhard bearing segments 226a-f to the support plate 222 may infiltrate the seams 236 and substantially fill all or a portion of the gaps at the seams 236, which may exist at the interfaces of the interior edge regions 234 of mating superhard bearing segments 226a-f. For example, suitable abrasion resistant braze alloys include, but are not limited to, silver-copper based braze alloys commercially known as braze 505 and braze 516 and are available from Handy & Harmon of Canada Limited. In another embodiment, a sealant material may comprise a hardfacing material (e.g., a nickel or cobalt alloy) applied at least within the gaps by thermal spraying. In yet a further embodiment, a sealant material may comprise polyurethane, or another suitable polymeric, metal, alloy, or other material. In another embodiment, a substantially continuous superhard bearing surface 216 may be at least partially formed by depositing a layer of diamond onto the surface 216 and into gaps between the segments 226a-f.
The superhard bearing segments 326a-d each may include an outer edge region 332 and an interior edge region 334. The superhard bearing segments 326a-d may be configured with a serrated geometry at the interior edge regions 334. Such a configuration may allow adjacent superhard bearing segments 326a-d to mate and at least partially interlock, while also defining seams 336 of a geometry that limits fluid leakage radially through the gaps between adjoining superhard bearing segments 326a-d.
The illustrated and described seams between adjacent superhard bearing segments are merely illustrative, and seams between superhard bearing segments and/or configurations of interior edge regions of superhard bearing segments may have any number of configurations. For, instance, a set of interconnecting superhard bearing segments may have substantially straight, serrated, saw-toothed, sinusoidal-like, curved, or otherwise shaped interior edge regions, or any combination of the foregoing. Moreover, some portions of an interior edge region may have one configuration of shape while another portion of an interior edge region on the same superhard bearing segment may have a different configuration or shape. Accordingly, different superhard bearing segments may also include different mating geometry or other configurations.
As discussed herein, a tilting pad bearing assembly may be utilized where certain conditions are met, or in any number of other circumstances or industries. For instance, an application may be identified where it would benefit to use a superhard bearing element including a superhard material; however, the superhard material may have associated production limits (e.g., size, availability, etc.). Where the superhard bearing element has a size, shape, or other feature(s) exceeding such production limits, the superhard bearing element may be fashioned out of multiple individual segments that collectively define a superhard bearing surface of the superhard bearing element. In other cases, however, the type of material used in the superhard bearing element may not have the same production limits as PDCs or other superhard materials, or the superhard bearing element may be sized small enough to allow a single superhard or other material to be used to form the superhard bearing surface.
Any of the above-described hydrodynamic tilting pad bearing assembly embodiments may be employed in a hydrodynamic tilting pad bearing apparatus.
The rotor 554 may be configured in any suitable manner, including in accordance with embodiments described herein. The rotor 554 may include a support ring 558 connected to one or more superhard bearing segments 562. The rotor 554 may include a substantially continuous superhard bearing surface which is generally adjacent the superhard bearing surfaces 516 of the stator 556. A fluid film may be formed between the substantially continuous superhard bearing surface of the rotor 554 and the superhard bearing surfaces 516 of the stator 556. In some embodiments, the superhard bearing surface of the rotor 554 may be formed of a single material and may be formed of a same or different material relative to materials used to form the tilting pad superhard bearing elements 504. In other embodiments, such as shown in
As shown in
The operation of the hydrodynamic tilting pad bearing apparatus 500 is discussed in more detail with reference to
The stator 556 may include tilting pads 504 that are optionally made of multiple segments 526. Moreover, in at least some embodiments, the tilting pads 504 may be configured to tilt as described herein. In such an embodiment, the tilting pads 504 may be positioned at a fixed tilt angle or at a configurable or self-establishing tilt angle. The tilting pads 504 of the stator 556 may have a leading edge 570 at a different position than a trailing edge 572 relative to the rotor 554. For instance, in
Under certain operational conditions, the pressure of the fluid film 568 may be sufficient to substantially prevent contact between the superhard bearing surfaces 560 of the rotor 554 and the superhard bearing surfaces 516 of the stator 556 and may thus substantially reduce wear of the superhard bearing segments 562 and the tilting pads 504. When the thrust loads exceed a certain value and/or the rotational speed of the rotor 554 is reduced, the pressure of the fluid film 568 may not be sufficient to substantially prevent the superhard bearing surfaces 560 of the rotor 554 and the superhard bearing surfaces 516 of the stator 556 from contacting each other. Under such operational conditions, the hydrodynamic tilting pad bearing apparatus 500 is not operated as a hydrodynamic bearing. Thus, under certain operational conditions, the hydrodynamic tilting pad bearing apparatus 500 may be operated as a hydrodynamic bearing apparatus and under other conditions the hydrodynamic tilting pad bear apparatus 500 may be operated so that the superhard bearing surfaces 516, 560 contact each other during use or a partially developed fluid film is present between the superhard bearing surfaces 516, 560. However, the tilting pads 504 and superhard bearing segments 562 may comprise superhard materials that are sufficiently wear-resistant to accommodate repetitive contact with each other, such as during start-up and shut-down of a subterranean drilling or other system employing the hydrodynamic tilting pad bearing apparatus 500 or other operational conditions not favorable for forming the fluid film 568. In still other embodiments, a backup roller or other bearing (not shown) may also be included for use during certain operational conditions, such as during start-up, or as the fluid film 558 develops.
An example manner in which the superhard bearing segments 562a, 562b may be assembled together is illustrated in
The interior edge sections 584 of the superhard bearing segments 562a, 562b may interconnect with, or otherwise correspond to, other of the multiple superhard bearing segments 562a, 562b. For instance, in the illustrated embodiment, each outer superhard bearing segment 562a may connect at opposing ends to other outer superhard bearing segments 562a that extend circumferentially relative thereto. Each outer superhard bearing segment 562a may also interface or mesh with one or more inner superhard bearing segment 562b which extend radially inward relative to the outer superhard bearing segment 562a. Such an arrangement is, however, merely exemplary. In other embodiments, there may be more than two superhard bearing segments extending radially to form the substantially continuous superhard bearing surface, any number of different segments extending circumferentially to form the substantially continuous superhard bearing surface, or a superhard bearing segment may interface with a segment extending at least partially in both circumferential and radial directions with respect thereto. Accordingly, a substantially continuous superhard bearing surface may be formed by a collective set of superhard bearing segments 562a, 562b each having a respective superhard bearing surfaces 560, and such superhard bearing segments 562a, 562b may be arranged, connected, or shaped in any suitable manner.
In
Accordingly regardless of the particular arrangement, multiple segments form the substantially continuous superhard bearing surface of the stator 556, a set of seams 582 may form between adjoining segments 562a, 562b. The seams 582 may provide a tortuous or winding path that limits fluid leakage radially through the seams 582. The seams 582 may correspond to a relatively small gap 580 existing between the segments 562a, 562b. Although not necessary, the size of the gaps 580 may be the same or similar to those described previously with respect to exemplary tilting pad superhard bearing elements. For instance, the gaps 580 may have a width of about 0.001 mm to about 3.5 mm, more particularly a width of about 0.0025 mm to about 2.5 mm, and more particularly a width of about 0.125 mm to about 1.25 mm. More particularly still, the gaps 580 may have a width from about 0.005 mm up to about 1.0 mm. The gaps 580 are optionally filled with a sealant material as described herein.
The concepts used in the hydrodynamic tilting pad bearing assemblies and apparatuses described herein may also be employed in tilting pad radial bearing assemblies and apparatuses.
The hydrodynamic tilting pad radial bearing apparatus 600 may further include an outer race 656 (e.g., a stator) configured to extend about and/or receive the inner race 654. The outer race 656 may include a plurality of circumferentially-spaced tilting pads 604, each of which may include a superhard bearing surface 616. The superhard bearing surface 616 may be substantially planar, although in other embodiments the superhard bearing surface 616 may be a concavely-curved superhard bearing surface to generally correspond to shapes of convexly-curved superhard bearing surfaces of the inner race 654. The terms “rotor” and “stator” refer to rotating and stationary components of the radial bearing system 600, respectively. Thus, if the inner race 654 is configured to remain stationary, the inner race 654 may be referred to as the stator and the outer race 656 may be referred to as the rotor.
The hydrodynamic tilting pad radial bearing apparatus 600 may be employed in a variety of mechanical applications. For example, rotary drill bits may benefit from a radial bearing apparatus disclosed herein. More specifically, the inner race 654 may be mounted or affixed to a spindle of a rotary drill bit and the outer race 656 may be affixed to an inner bore such that an outer race 656 and inner race 654 may be assembled to form the radial bearing system 600.
With continued reference to
As further illustrated in
Each superhard bearing surface 616 of a corresponding tilting pad 604 may be tilted in a manner that facilities sweeping in of a lubricant or other fluid to form a fluid film between the inner race 654 and the outer race 656. Each tilting pad 604 may be tilted and/or tilt about an axis that is generally parallel to the central axis 606. As a result, each tilting pad 604 may be tilted at an angle relative to the inner and outer surfaces of the ring 602 and in a circumferential fashion such that the leading edges 670 of the tilting pads 604 are about parallel to the central axis 606. The leading edge 670 may help to sweep lubricant or another fluid onto the superhard bearing surfaces 616 of the stator 656 to form a fluid film in a manner similar to the tilting pads 504 shown in
In some embodiments, the tilting pad 604 may be formed from a plurality of superhard bearing segments 626 that collectively define a respective tilting pad 604 and/or superhard bearing surface 616. Each superhard bearing segment 626 may be substantially identical, or the superhard bearing segments 626 may be different relative to other of the superhard bearing segments 626. In some embodiments, the superhard bearing segments 626 each include a superhard table 618 bonded to a substrate 620 as described herein. Optionally, the substrate 620 may be connected or supported relative to a support plate 622, the support ring 602, or other material or component. The support plate 622 may be a single component or segment and used to facilitate assembly of the multiple segments 626 into the superhard bearing element 604, although in other embodiments the support plate 622 may also include multiple assembled segments.
With continued reference to
As further illustrated in
As noted previously, the plurality of superhard bearing segments 662 may be distributed circumferentially and/or longitudinally relative to the axis 606. Where the superhard bearing segments 662 include a superhard table 674 and/or a substrate 676, the superhard tables 674 and substrates 676 may be fabricated from the same materials described above for the superhard bearing segments 104 shown in
The support ring 658 of the inner race 654 may include a circumferentially extending recess configured to receive the plurality of superhard bearing segments 662. The superhard bearing segments 662 may be secured within the recess or otherwise secured to the support ring 658 by brazing, press-fitting, using fasteners, or another suitable technique. The support ring 658 may also define an interior surface 667 defining an opening 655 that is capable of receiving, for example, a shaft of a motor from a downhole motor assembly or other apparatus.
Any of the embodiments for bearing apparatuses discussed above may be used in a subterranean drilling system.
The tilting pad bearing apparatus 701 may include a stator 756 that does not rotate and a rotor 754 that may be attached to the output shaft 706 and may rotate with the output shaft 706. The rotor 754 optionally includes a plurality of adjacent superhard bearing segments (not shown) assembled together to form a substantially continuous superhard bearing element, as previously described such as in the stator 654 shown in
In operation, drilling or other fluid may be circulated through the downhole drilling motor 724 to generate torque and effect rotation of the output shaft 706 and the rotary drill bit 712 attached thereto so that a borehole may be drilled. A portion of the fluid may also be used to lubricate opposing superhard bearing surfaces of the stator 756 and rotor 754. When the rotor 754 is rotated at a sufficient rotational speed, the fluid may be swept onto the superhard bearing surfaces of the stator 756 and a fluid film having sufficient pressure may develop that maintains the superhard bearing surfaces of the stator 756 and the superhard bearing surfaces of the rotor 754 apart, as previously discussed. In embodiments in which the superhard bearing surfaces of the stator 756 are tilted such as in the case of example tilting pad bearing assemblies, the tilted superhard bearing surfaces may facilitate formation of a film thickness having different thicknesses at leading and trailing edges of the superhard bearing elements 704.
Although the bearing assemblies and apparatuses described above have been discussed in the context of subterranean drilling systems and applications, in other embodiments, the bearing assemblies and apparatuses disclosed herein are not limited to such use and may be used for many different applications, if desired, without limitation. Thus, such bearing assemblies and apparatuses are not limited for use with subterranean drilling systems and may be used with various other mechanical systems, without limitation.
While various aspects and embodiments have been disclosed herein, other aspects and embodiments are contemplated. The various aspects and embodiments disclosed herein are for purposes of illustration and are not intended to be limiting. Additionally, the words “including,” “having,” and variants thereof (e.g., “includes” and “has”) as used herein, including the claims, shall be open ended and have the same meaning as the word “comprising” and variants thereof (e.g., “comprise” and “comprises”).
Cooley, Craig H., Sexton, Timothy N.
Patent | Priority | Assignee | Title |
10054154, | Apr 19 2011 | US Synthetic Corporation | Bearing apparatus including tilting pads |
10570953, | Apr 19 2011 | US Synthetic Corporation | Bearing apparatus including tilting pads |
10711792, | Oct 01 2015 | THERMODYN SAS | Auxiliary turbomachinery shaft support system and turbomachinery comprising said system |
11009071, | Jun 07 2017 | US Synthetic Corporation | Bearing assemblies, related bearing apparatuses, and related methods |
11015646, | Apr 19 2011 | US Synthetic Corportation | Bearing apparatus including tilting pads |
11512533, | Jun 07 2017 | US Synthetic Corporation | Bearing assemblies, related bearing apparatuses, and related methods |
8967871, | Apr 19 2011 | US Synthetic Corporation | Bearing assemblies and apparatuses including tilting superhard bearing elements, and motor assemblies using the same |
8967872, | Apr 19 2011 | US Synthetic Corporation | Bearing assemblies, and related methods |
9255605, | Apr 19 2011 | US Synthetic Corporation | Bearing assemblies and apparatuses including tilting superhard bearing elements, and motor assemblies using the same |
9429188, | Apr 19 2011 | US Synthetic Corporation | Bearing assemblies, and related methods |
9702400, | Apr 19 2011 | US Synthetic Corporation | Bearing apparatuses including tilting pads and methods of operating such bearing apparatuses |
D888787, | Jun 07 2017 | US Synthetic Corporation | Radial bearing |
D888788, | Jun 07 2017 | US Synthetic Corporation | Radial bearing |
ER4090, | |||
ER9608, |
Patent | Priority | Assignee | Title |
3817586, | |||
3887245, | |||
4077682, | Aug 24 1976 | DELAWARE CAPITAL FORMATION, INC , 1100 NORTH MARKET STREET, SUITE 780, WILMINGTON, DE , 19801, A CORP OF DE | Large thrust bearing with lubrication in the spaces between pads |
4097094, | Aug 24 1976 | DELAWARE CAPITAL FORMATION, INC , 1100 NORTH MARKET STREET, SUITE 780, WILMINGTON, DE , 19801, A CORP OF DE | Journal bearing assembly with flexible support and viscous damping |
4268276, | Apr 25 1978 | General Electric Company | Compact of boron-doped diamond and method for making same |
4274900, | Aug 30 1978 | CRYOVAC, INC | Multi-layer polyester/polyolefin shrink film |
4296976, | Apr 03 1980 | Mechanical Technology Incorporated | Cross-plies support element for compliant bearings |
4403873, | Jan 11 1982 | DELAWARE CAPITAL FORMATION, INC , 1100 NORTH MARKET STREET, SUITE 780, WILMINGTON, DE , 19801, A CORP OF DE | Tilting pad thrust bearing |
4410054, | Dec 03 1981 | Maurer Engineering Inc. | Well drilling tool with diamond radial/thrust bearings |
4468138, | Sep 28 1981 | Maurer Engineering Inc. | Manufacture of diamond bearings |
4501505, | Jun 06 1984 | KINGSBURY, INC , 10385 DRUMMOND ROAD, PHILADELPHIA, PA 19154 A CORP OF | Thrust bearing |
4525083, | Aug 31 1981 | General Electric Company; GENERAL ELECTRIC COMPANY A NY CORP | Trimetallic bearings |
4544285, | Apr 18 1983 | The United States of America as represented by the Secretary of the Navy; United States of America as represented by the Secretary of the Navy | Fluid equalized tilting pad thrust bearings |
4560014, | Apr 05 1982 | Halliburton Company | Thrust bearing assembly for a downhole drill motor |
4662348, | Jun 20 1985 | SII MEGADIAMOND, INC | Burnishing diamond |
4720199, | Sep 03 1986 | Halliburton Company | Bearing structure for downhole motors |
4729440, | Apr 16 1984 | Smith International, Inc | Transistion layer polycrystalline diamond bearing |
4738322, | Dec 20 1984 | SMITH INTERNATIONAL, INC , IRVINE, CA A CORP OF DE | Polycrystalline diamond bearing system for a roller cone rock bit |
4738550, | Sep 08 1986 | Delaware Capital Formation, Inc | Tilting pad thrust bearing with optimized tilt axis location |
4756631, | Jul 24 1987 | Smith International, Inc. | Diamond bearing for high-speed drag bits |
4764036, | May 14 1987 | Halliburton Company | PCD enhanced radial bearing |
4811801, | Mar 16 1988 | SMITH INTERNATIONAL, INC , A DELAWARE CORPORATION | Rock bits and inserts therefor |
4824263, | Apr 15 1983 | DRESSER-RAND COMPANY, CORNING, NEW YORK A GENERAL PARTNERSHIP OF NEW YORK | Thrust bearing shoes |
4913247, | Jun 09 1988 | EASTMAN CHRISTENSEN COMPANY, A CORP OF DE | Drill bit having improved cutter configuration |
4927275, | Sep 23 1988 | The Torrington Company | Equalizing hydrodynamic bearing |
5016718, | Jan 26 1989 | Geir, Tandberg; Arild, Rodland | Combination drill bit |
5092687, | Jun 04 1991 | Anadrill, Inc. | Diamond thrust bearing and method for manufacturing same |
5120327, | Mar 05 1991 | Halliburton Energy Services, Inc | Cutting composite formed of cemented carbide substrate and diamond layer |
5135061, | Aug 04 1989 | Reedhycalog UK Limited | Cutting elements for rotary drill bits |
5137373, | Oct 25 1988 | KMC BEARINGS, INC | Bearings having beam mounted bearing pads and methods of making same |
5154245, | Apr 19 1990 | SANDVIK AB, A CORP OF SWEDEN | Diamond rock tools for percussive and rotary crushing rock drilling |
5180022, | May 23 1991 | DOVER BMCS ACQUISITION CORP | Rotary mining tools |
5364192, | Oct 28 1992 | Diamond bearing assembly | |
5368398, | Oct 28 1992 | CSIR | Diamond bearing assembly |
5393145, | May 29 1987 | Waukesha Bearings Corporation | Pad type hydrodynamic thrust bearings having a modular construction |
5460233, | Mar 30 1993 | Baker Hughes Incorporated | Diamond cutting structure for drilling hard subterranean formations |
5480233, | Oct 14 1994 | Thrust bearing for use in downhole drilling systems | |
5544713, | Aug 17 1993 | Dennis Tool Company | Cutting element for drill bits |
6736542, | Aug 15 2002 | General Electric Company | Reduced width tilting pad journal bearing and related method |
6793681, | Aug 12 1994 | DIMICRON, INC | Prosthetic hip joint having a polycrystalline diamond articulation surface and a plurality of substrate layers |
7060641, | May 30 2003 | Triad National Security, LLC | Diamond-silicon carbide composite |
7533739, | Jun 09 2005 | US Synthetic Corporation | Cutting element apparatuses and drill bits so equipped |
7552782, | Nov 02 2006 | US Synthetic Corporation | Thrust-bearing assembly |
7635035, | Aug 24 2005 | US Synthetic Corporation | Polycrystalline diamond compact (PDC) cutting element having multiple catalytic elements |
7866418, | Oct 03 2008 | US Synthetic Corporation | Rotary drill bit including polycrystalline diamond cutting elements |
7870913, | Jul 18 2007 | US Synthetic Corporation | Bearing assemblies, and bearing apparatuses and motor assemblies using same |
7901137, | Jan 11 2008 | US Synthetic Corporation | Bearing assembly, and bearing apparatus and motor assembly using same |
7942218, | Jun 09 2005 | US Synthetic Corporation | Cutting element apparatuses and drill bits so equipped |
8118117, | Jun 09 2005 | CERADYNE, INC | Thrust bearing assembly |
8146687, | Feb 09 2009 | US Synthetic Corporation | Polycrystalline diamond compact including at least one thermally-stable polycrystalline diamond body and applications therefor |
8236074, | Oct 10 2006 | US Synthetic Corporation | Superabrasive elements, methods of manufacturing, and drill bits including same |
20030012468, | |||
20040190804, | |||
20070046120, | |||
20100264134, | |||
20100288558, | |||
20110174544, | |||
20120241224, | |||
20120261197, | |||
KR748595, |
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